Airbus A320neo vs. Airbus H225 Super Puma
... or view the full comparison list
here.
Airbus A320neo |
versus |
Airbus H225 Super Puma |
37.57 m |
123 ft 3 in |
length |
14.06 m |
46 ft 2 in |
11.76 m |
38 ft 7 in |
height |
4.38 m |
14 ft 4 in |
35.8 m |
117 ft 5 in |
wingspan |
|
|
2 x PW 1100G or 2 x CFM LEAP-1A |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
120kN (PW 1100G) or 109-156kN (CFM LEAP-1A) |
thrust per engine |
2,778 hp |
240kN (PW 1100G) or 218-312kN (CFM LEAP-1A) |
total thrust |
5,556 hp |
79,000 kg |
174,200 lb |
MTOW |
11,000 kg |
24,251 lb |
6,300 km |
3,403 nm |
range |
857 km |
463 nm |
M0.82 |
101,3 km/h |
cruise speed |
242 km/h |
150 mph |
150-180 |
capacity |
24-28 |
|
|
rotor diameter |
16.2 m |
53 ft 2 in |
|
|
rate of climb |
10.7 m/s |
2,106 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.